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时间:2011-03-27 08:55来源:蓝天飞行翻译 作者:admin
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 1EFF : ALL 1 55-32-11Page 408 1 1 May 01/05R 1 1 1CES 1


 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific vacuum pump R No specific Torque Wrench : range 0.00 to 1.20 m.daN R (0.00 to 9.00 lbf.ft)
 98D55307531001 1 SLING - DORSAL FIN, LEADING EDGES, END CAP
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 05-013A  C Z-24.223
 RELEASE AGENT (Ref. 20-31-00)

 Material No. 05-052 SELF-ADHES.PVC DISKS FOR HOISTING POINT BLANKING (Ref. 20-31-00)
 Material No. 08-065 USA MIL-T-60394 TYPE I CLASS I DOUBLE SIDED ADHESIVE TAPE (Ref. 20-31-00) Material No. 09-005 USA MIL-S-81733 CLASS C CORROSION INHIBITIVE INTERFAY SEALANT (Ref. 20-31-00)
 Material No. 09-013  USA MIL-PRF-81733 TYPE I CLASS A
 CORROSION INHIBITING BRUSH CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-016  USA MIL-PRF-81733D TYPE II CLASS B
 CORROSION INHIBITING FILLET CONSISTENCY
 (Ref. 20-31-00)

 Material No. 09-018  USA AMS 3267/3
 CORROSION INHIBITING LOW ADHESION SEALANT
 (Ref. 20-31-00)

 Material No. 09-030  D 80-T-50-4005
 SEAL TAPE (Ref. 20-31-00)

 Material No. 11-004  USA MIL-T-81533
 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM)
 (Ref. 20-31-00)

 Material No. 11-008
 (USE 11-008A) (Ref. 20-31-00)

 

 C. Referenced Information

 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
20-28-00-912-004  Electrical Bonding of Components With Conductive Bolts and Screws and Bonding Straps in the Fuselage and in the Wings (this does not include the tanks)-
29-00-00-864-001 Put the Related Hydraulic System in the Depressurized Configuration before Maintenance Action ASRM 512300

R **ON A/C 001-049, 101-149, 151-199, 201-299, 301-399, 401-499,
 55-32-11-991-001-A  Fig. 401
 **ON A/C 051-099,
 55-32-11-991-001  Fig. 401A
 **ON A/C 001-049, 101-105, 201-203,
 55-32-11-991-003  Fig. 402
 **ON A/C ALL
 3. Job Set-up
__________
 Subtask 55-32-11-860-050

 A. Aircraft Maintenance Configuration
 (1)
 Make sure that the warning notices are in position to tell persons not to operate the flight controls.

 (2)
 Make sure that the Green, Blue and Yellow system is depressurized (Ref. TASK 29-00-00-864-001).

 (3)
 Make sure that the access platform is in position.

 


 Subtask 55-32-11-865-053

 B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/THS/ACTR/MOT2 19CE2 B09 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU AUTO FLT/FAC1/28VDC 5CC1 B04 49VU AUTO FLT/FAC1/26VAC 14CC1 B03 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU AUTO FLT/RUDDER/TRIM/IND 15CC M20 121VU AUTO FLT/FAC2/28VDC 5CC2 M19 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20

R **ON A/C 001-049, 101-105, 201-203,
 Subtask 55-32-11-560-050-A
 C. Preparation for Installation
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL
_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 (Ref. Fig. 402/TASK 55-32-11-991-003)


 (1) Prepare the vertical stabilizer leading-edge for installation.

 (a)
 Remove the old sealant from the mating surface of the leading edge sections, the ribs and the spar box with a nonmetallic scraper.

 (b)
 Make sure that the anchor nuts at the leading edge ribs and along the spar box are in good condition.
 
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